Research on MHD heat shield effect under flight condition
| Project/Area Number |
26820378
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| Research Category |
Grant-in-Aid for Young Scientists (B)
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| Allocation Type | Multi-year Fund |
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| Research Field |
Aerospace engineering
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| Research Institution | Okayama University |
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Principal Investigator |
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| Research Collaborator |
YUHARA Shota
MUTA Masayuki
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| Project Period (FY) |
2014-04-01 – 2017-03-31
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| Project Status |
Completed (Fiscal Year 2016)
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| Budget Amount *help |
¥3,900,000 (Direct Cost: ¥3,000,000、Indirect Cost: ¥900,000)
Fiscal Year 2016: ¥780,000 (Direct Cost: ¥600,000、Indirect Cost: ¥180,000)
Fiscal Year 2015: ¥780,000 (Direct Cost: ¥600,000、Indirect Cost: ¥180,000)
Fiscal Year 2014: ¥2,340,000 (Direct Cost: ¥1,800,000、Indirect Cost: ¥540,000)
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| Keywords | 航空宇宙工学 / 大気圏再突入機 / プラズマ流制御 / 電磁流体 / 熱防御システム |
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| Outline of Final Research Achievements |
MHD heat shield is an innovative technology to protect the vehicle from severe heating during atmospheric entry flight to return from the space. In this research, the MHD heat shield effect was experimentally measured under air plasma flow to improve the numerical prediction. As a result, new measurement device was developed and it was confirmed that the MHD heat shield effect is also generated under the air plasma flow.
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Report
(4 results)
Research Products
(5 results)
